학술논문

Software-Defined Architecture and Front-End Optimization for DO-178B Compliant Distance Measuring Equipment
Document Type
Conference
Source
2023 Integrated Communication, Navigation and Surveillance Conference (ICNS) Integrated Communication, Navigation and Surveillance Conference (ICNS), 2023. :1-9 Apr, 2023
Subject
Aerospace
Communication, Networking and Broadcast Technologies
Computing and Processing
Robotics and Control Systems
Signal Processing and Analysis
Transportation
Radio transmitters
Power amplifiers
Radio navigation
Computer architecture
Aerospace electronics
Software
Transponders
Standards
Optimization
Guidelines
software defined radio
DME
distance measuring equipment
avionics
DO-178
Language
ISSN
2155-4951
Abstract
Among the air navigation technologies, many of them are capable of increasing the aviation sustainability as well as accuracy improvement in Alternative Positioning, Navigation, and Timing (APNT) specially avionics Distance Measuring Equipment (DME), Very high frequency Omni-directional Range (VOR), etc. The integration of these air navigation solutions could make a robust and efficient accuracy in air mobility, air traffic management and autonomous operations. Designing a proper RF front-end, power amplifier and software-defined transponder could pave the way of reaching an optimized avionics navigation solution. In this article, the possibility of reaching an optimum front-end to be used with single low-cost Software-Defined Radio (SDR) has been investigated in order to reach a novel software-defined DME architecture. Our software-defined approach uses the firmware possibilities to design a real-time software architecture compatible with a Multi Input Multi Output (MIMO) BladeRF to estimate an accurate time delay between a Transmission (Tx) and the reception (Rx) channels using the synchronous scheduled communication. We could design a novel power amplifier for the transmission channel of the DME to pass the minimum transmission power. This article also investigates designing a proper pair pulse based on the DO-178B avionics standard. Various guidelines have been tested and the possibility of passing the certification process for each standard term have been analyzed. Finally, the performance of the DME has been tested in the laboratory environment using an IFR6000 which showed that the proposed architecture reached the accuracy of less than 0.23 Nautical mile (Nmi) with 98% probability.